View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 47791U 26145.56713867 +.00000000 +00000-0 +24196-4 0 00008
2 47791 53.1572 245.3622 0001033 91.2363 268.8757 15.31705997 08
| Epoch (UTC): | 25 May 2026 13:36:40 |
| Eccentricity: | 0.0001033 |
| inclination: | 53.1572° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 245.3622° |
| argument of perigee: | 91.2363° |
| revolutions per day: | 15.31705997 |
| mean anomaly at epoch: | 268.8757° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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